Wind Tunnel Pressure Distribution Tests on a Series of Biplane Wing Models Part I: Effects of Changes in Stagger and Gap Page: 27 of 34
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4100 0o 100 200 300 400 500
Angle of attack, L600 700 800 900
Fig.16 Effect of gap on cellule normal. force coefficient.
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Knight, Montgomery & Noyes, Richard W. Wind Tunnel Pressure Distribution Tests on a Series of Biplane Wing Models Part I: Effects of Changes in Stagger and Gap, report, July 1929; (https://digital.library.unt.edu/ark:/67531/metadc54010/m1/27/: accessed May 10, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.